11/21/25
Message Overview:
Message Name:
[CPC1] OUTFLOW VALVE #1
Message Code:
2137317ABG
Associated CAS:
| Reporting LRU: | Cabin Pressure Controller 1 |
| System Description: | 21-31-00- Cabin Pressure Control System |
| Schematic Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] 21-31-00 Cabin Pressure Control System |
| Wiring Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] 21-31-0 3 Cabin Pressure Control System |
Message Description:
During PBIT, the Outflow Valve (OFV) 1 does not respond to test command from Cabin Pressure Controller (CPC) 1. Inhibited during Take-off and Landing.
Possible Causes:
- Cabin Pressure Controller (CPC) 1 (A21)
- FWD Outflow Valve (OFV) 1 (L8)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None
Flight Operation Notifications Manual (FONM): None
NOTES:
- CPC in control alternate between CPC 1 and CPC 2
- CPC1 is used for odd days.
- CPC2 is used for even days
Quick Links:
| Removal of the Cabin Pressure Controllers | AMM 21-31-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Cabin Pressure Controllers | AMM 21-31-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Outflow Valves | AMM 21-31-05-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Outflow Valves | AMM 21-31-05-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Initiate an IBIT from CPC1. (CPC1 is used for odd days. CPC2 is used for even days). If test passes with CPC1, Interchange CPC1 and CPC2. If problem follows, replace the defective LRU.
- Perform wiring checks between CPC1 (A21P1) and Outflow valve 1 (L8P1).
- If wiring checks are not good, repair defective associated wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring checks between CPC 1 and the cockpit Pressurization Control Panel using SSM 21-31-00.
- If wiring checks are not good, repair defective associated wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Using SSM 21-31-00, perform wiring checks on the cockpit Pressurization Control Panel side of connectors AP9J1 and AP9J2. Make sure to check Outflow Valve 1 pushbutton (SDS2), Dump Relay 1 (K1) and ALT Limit Relay 1 (K2) for proper operation.
- If defects are found, repair/replace defective component as required.
- If checks are good, continue with next step.
- Replace Outflow Valve 1.
- Do close out.